Fracture mechanics correlation for tensile failure of filamentary composites with holes
- 1 July 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (7) , 703-704
- https://doi.org/10.2514/3.44618
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Finite element analysis of stress intensity factors for cracks at a bi-material interfaceInternational Journal of Fracture, 1976
- Uniaxial Failure of Composite Laminates Containing Stress ConcentrationsPublished by ASTM International ,1975
- Stress Fracture Criteria for Laminated Composites Containing Stress ConcentrationsJournal of Composite Materials, 1974
- Structural optimization for aeroelastic requirementsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Macroscopic Fracture Mechanics of Advanced Composite MaterialsJournal of Composite Materials, 1971
- Crack Point Stress Singularities at a Bi-Material InterfaceJournal of Applied Mechanics, 1963